Console Output

Skipping 454 KB.. Full Log
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  4.5532e+00|   -0.176079|    2.186024|    1.926491|    5.314817|    1.968491|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.5418e+00|   -0.097023|    2.377425|    2.077233|    5.406914|    2.695550|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.3027e+00|   -0.019814|    2.508051|    2.361192|    5.481501|    4.194649|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.1468e+00|   -0.057509|    2.546491|    2.502868|    5.427676|    6.178612|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.1491e+00|   -0.105546|    2.541254|    2.542658|    5.365316|    7.839149|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  4.0894e+00|   -0.116723|    2.527854|    2.543233|    5.363987|    9.027832|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  4.0232e+00|   -0.132260|    2.491265|    2.536291|    5.352665|    9.934088|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  3.9481e+00|   -0.169378|    2.422959|    2.526207|    5.306584|   10.491937|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  3.9085e+00|   -0.225151|    2.344318|    2.503017|    5.236605|   10.611804|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  3.8895e+00|   -0.276476|    2.300459|    2.458641|    5.181642|   10.402339|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.276476|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).

------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  0.797978 Cd =  0.076711
Cmx =  -0.000504 Cmy =  -0.202445 Cmz =  -0.000108
Cx =  0.062773 Cy =  -0.000218 Cz =  0.799195
Pressure Contribution
Cl_p =  0.797978 Cd_p =  0.076711
Cmx_p =  -0.000504 Cmy_p =  -0.202445 Cmz_p =  -0.000108
Cx_p =  0.062773 Cy_p =  -0.000218 Cz_p =  0.799195
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmx_v =  0.0 Cmy_v =  0.0 Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0 Cz_v =  0.0
==3713034== 
==3713034== HEAP SUMMARY:
==3713034==     in use at exit: 4,310,578 bytes in 24,768 blocks
==3713034==   total heap usage: 1,492,037 allocs, 1,467,269 frees, 1,450,118,077 bytes allocated
==3713034== 
==3713034== LEAK SUMMARY:
==3713034==    definitely lost: 0 bytes in 0 blocks
==3713034==    indirectly lost: 0 bytes in 0 blocks
==3713034==      possibly lost: 0 bytes in 0 blocks
==3713034==    still reachable: 0 bytes in 0 blocks
==3713034==         suppressed: 4,310,578 bytes in 24,768 blocks
==3713034== 
==3713034== For lists of detected and suppressed errors, rerun with: -s
==3713034== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1840 from 1840)
492.50user 4.19system 8:18.68elapsed 99%CPU (0avgtext+0avgdata 814728maxresident)k
168inputs+139688outputs (1major+1061763minor)pagefaults 0swaps

real	8m18.689s
user	8m12.513s
sys	0m4.196s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==3773987== Memcheck, a memory error detector
==3773987== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==3773987== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==3773987== Command: python -u su2_and_Delaundo_PyTest.py -outLevel=0
==3773987== 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes be in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundoMesh.mesh
	Swapping y and z coordinates!

Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file


Writing SU2 file ....
SU2 expects 2D meshes be in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Warning: No boundary condition specified for capsGroup 2DSlice!
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.1) "


Running SU2......
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='delaundoMesh.cfg' mode='r' encoding='UTF-8'>
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==3788740== Warning: invalid file descriptor 1048564 in syscall close()
==3788740== Warning: invalid file descriptor 1048565 in syscall close()
==3788740== Warning: invalid file descriptor 1048566 in syscall close()
==3788740== Warning: invalid file descriptor 1048567 in syscall close()
==3788740==    Use --log-fd=<number> to select an alternative log fd.
==3788740== Warning: invalid file descriptor 1048568 in syscall close()
==3788740== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundoMesh.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_delaundoMesh.dat.
Surface file name: surface_flow_delaundoMesh.
Volume file name: flow_delaundoMesh.
Restart file name: restart_flow_delaundoMesh.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
6320 grid points.
12346 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12346 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        45.3524|        89.3051|
|     CV Face Area Aspect Ratio|         1.0235|        15.7138|
|           CV Sub-Volume Ratio|              1|        7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      6320|    1/1.00|        10|
|         1|      1790|    1/3.53|   7.98287|
|         2|       504|    1/3.55|   6.35388|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.4996e-01|   -1.163171|    1.073770|    1.341444|    4.312165|    0.062120|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.4888e-01|   -1.561828|    0.808636|    0.967487|    3.922716|    0.139775|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.4824e-01|   -1.601698|    0.943793|    1.009036|    3.876382|    0.373708|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.4783e-01|   -1.659374|    1.008221|    1.015635|    3.799753|    0.952935|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.4704e-01|   -1.663585|    1.011627|    0.956487|    3.788246|    2.344781|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.4548e-01|   -1.633451|    0.991734|    0.872954|    3.829708|    6.259549|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.4440e-01|   -1.626398|    0.990123|    0.847075|    3.843511|   26.349557|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.4264e-01|   -1.643439|    1.009125|    0.895796|    3.825758|  -56.104873|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.4022e-01|   -1.659565|    1.020774|    0.939260|    3.804302|  -24.431167|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.4001e-01|   -1.676757|    1.012633|    0.938320|    3.783310|  -21.456834|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.67676|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_delaundoMesh.dat      |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|CSV file                           |surface_flow_delaundoMesh.csv      |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary                     |flow_delaundoMesh.szplt            |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary surface             |surface_flow_delaundoMesh.szplt    |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).

------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  0.805231 Cd =  -0.037528
Cmz =  0.414714
Cx =  -0.037528 Cy =  0.805231
Pressure Contribution
Cl_p =  0.805231 Cd_p =  -0.037528
Cmz_p =  0.414714
Cx_p =  -0.037528 Cy_p =  0.805231
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0
==3773987== 
==3773987== HEAP SUMMARY:
==3773987==     in use at exit: 4,286,199 bytes in 24,705 blocks
==3773987==   total heap usage: 650,978 allocs, 626,273 frees, 384,807,853 bytes allocated
==3773987== 
==3773987== LEAK SUMMARY:
==3773987==    definitely lost: 0 bytes in 0 blocks
==3773987==    indirectly lost: 0 bytes in 0 blocks
==3773987==      possibly lost: 0 bytes in 0 blocks
==3773987==    still reachable: 0 bytes in 0 blocks
==3773987==         suppressed: 4,286,199 bytes in 24,705 blocks
==3773987== 
==3773987== For lists of detected and suppressed errors, rerun with: -s
==3773987== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1862 from 1862)
61.13user 1.54system 1:03.19elapsed 99%CPU (0avgtext+0avgdata 464212maxresident)k
32inputs+15056outputs (1major+323027minor)pagefaults 0swaps

real	1m3.202s
user	1m1.136s
sys	0m1.553s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_and_pointwise_PyTest.py test;'
su2_and_pointwise_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==3789150== Memcheck, a memory error detector
==3789150== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==3789150== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==3789150== Command: python -u su2_and_pointwise_PyTest.py -outLevel=0
==3789150== 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
Number of command line arguments = 2
Sat Jul 02 2022  6:58:38AM EDT
Pointwise V18.5
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 10
    MaxDim                   = 15
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
  Quilt list has 18 entries.
  Quilt quilt-1: edge tolerance = 6.19984e-05
  Quilt quilt-2: edge tolerance = 6.19984e-05
  Quilt quilt-3: edge tolerance = 6.19984e-05
  Quilt quilt-4: edge tolerance = 6.19984e-05
  Quilt quilt-5: edge tolerance = 6.19984e-05
  Quilt quilt-6: edge tolerance = 6.19984e-05
  Quilt quilt-7: edge tolerance = 6.19984e-05
  Quilt quilt-8: edge tolerance = 6.19984e-05
  Quilt quilt-9: edge tolerance = 8.32902e-05
  Quilt quilt-10: edge tolerance = 8.32902e-05
  Quilt quilt-11: edge tolerance = 8.32902e-05
  Quilt quilt-12: edge tolerance = 8.32902e-05
  Quilt quilt-13: edge tolerance = 8.32902e-05
  Quilt quilt-14: edge tolerance = 8.32902e-05
  Quilt quilt-15: edge tolerance = 8.32902e-05
  Quilt quilt-16: edge tolerance = 8.32902e-05
  Quilt quilt-17: edge tolerance = 6.19601e-06
  Quilt quilt-18: edge tolerance = 6.19601e-06
  Maximum DB edge tolerance = 8.32902e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.665804e-04 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 18 entries.
Quilt list has 18 entries.
Original connector list has 32 entries.
Minimum connector length = 0.00316783
Tolerance = 8.32902e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 32 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-12
Max Edge Tol: 8.329e-05 on con-23
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/32, name = con-1
  Changing dimension for connector 1/32 from 10 to 4
Checking dimension for connector 2/32, name = con-2
Checking dimension for connector 3/32, name = con-3
  Changing dimension for connector 3/32 from 10 to 3
Checking dimension for connector 4/32, name = con-4
Checking dimension for connector 5/32, name = con-5
  Changing dimension for connector 5/32 from 10 to 3
Checking dimension for connector 6/32, name = con-6
  Changing dimension for connector 6/32 from 10 to 3
Checking dimension for connector 7/32, name = con-7
  Changing dimension for connector 7/32 from 10 to 3
Checking dimension for connector 8/32, name = con-8
Checking dimension for connector 9/32, name = con-9
  Changing dimension for connector 9/32 from 10 to 4
Checking dimension for connector 10/32, name = con-10
Checking dimension for connector 11/32, name = con-12
  Changing dimension for connector 11/32 from 10 to 3
Checking dimension for connector 12/32, name = con-13
Checking dimension for connector 13/32, name = con-16
  Changing dimension for connector 13/32 from 10 to 3
Checking dimension for connector 14/32, name = con-17
Checking dimension for connector 15/32, name = con-20
  Changing dimension for connector 15/32 from 10 to 3
Checking dimension for connector 16/32, name = con-21
  Changing dimension for connector 16/32 from 10 to 4
Checking dimension for connector 17/32, name = con-22
Checking dimension for connector 18/32, name = con-23
  Changing dimension for connector 18/32 from 10 to 3
Checking dimension for connector 19/32, name = con-24
Checking dimension for connector 20/32, name = con-25
  Changing dimension for connector 20/32 from 10 to 3
Checking dimension for connector 21/32, name = con-26
  Changing dimension for connector 21/32 from 10 to 3
Checking dimension for connector 22/32, name = con-27
  Changing dimension for connector 22/32 from 10 to 3
Checking dimension for connector 23/32, name = con-28
Checking dimension for connector 24/32, name = con-29
  Changing dimension for connector 24/32 from 10 to 4
Checking dimension for connector 25/32, name = con-30
Checking dimension for connector 26/32, name = con-32
  Changing dimension for connector 26/32 from 10 to 3
Checking dimension for connector 27/32, name = con-33
Checking dimension for connector 28/32, name = con-36
  Changing dimension for connector 28/32 from 10 to 3
Checking dimension for connector 29/32, name = con-37
Checking dimension for connector 30/32, name = con-40
  Changing dimension for connector 30/32 from 10 to 3
Checking dimension for connector 31/32, name = con-41
Checking dimension for connector 32/32, name = con-42
Processing spacing values for connector 1/32, name = con-1
Processing spacing values for connector 2/32, name = con-2
Processing spacing values for connector 3/32, name = con-3
Processing spacing values for connector 4/32, name = con-4
Processing spacing values for connector 5/32, name = con-5
Processing spacing values for connector 6/32, name = con-6
Processing spacing values for connector 7/32, name = con-7
Processing spacing values for connector 8/32, name = con-8
Processing spacing values for connector 9/32, name = con-9
Processing spacing values for connector 10/32, name = con-10
Processing spacing values for connector 11/32, name = con-12
Processing spacing values for connector 12/32, name = con-13
Processing spacing values for connector 13/32, name = con-16
Processing spacing values for connector 14/32, name = con-17
Processing spacing values for connector 15/32, name = con-20
Processing spacing values for connector 16/32, name = con-21
Processing spacing values for connector 17/32, name = con-22
Processing spacing values for connector 18/32, name = con-23
Processing spacing values for connector 19/32, name = con-24
Processing spacing values for connector 20/32, name = con-25
Processing spacing values for connector 21/32, name = con-26
Processing spacing values for connector 22/32, name = con-27
Processing spacing values for connector 23/32, name = con-28
Processing spacing values for connector 24/32, name = con-29
Processing spacing values for connector 25/32, name = con-30
Processing spacing values for connector 26/32, name = con-32
Processing spacing values for connector 27/32, name = con-33
Processing spacing values for connector 28/32, name = con-36
Processing spacing values for connector 29/32, name = con-37
Processing spacing values for connector 30/32, name = con-40
Processing spacing values for connector 31/32, name = con-41
Processing spacing values for connector 32/32, name = con-42
Number of unique endpoints = 20
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/32, con-1.
    Connector dimension changed from 4 to 15, avg. spacing changed from 1.33869 to 0.286862
  Proximity test for connector 2/32, con-2.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
  Proximity test for connector 3/32, con-3.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
  Proximity test for connector 4/32, con-4.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
  Proximity test for connector 5/32, con-5.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
  Proximity test for connector 6/32, con-6.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
  Proximity test for connector 7/32, con-7.
  Proximity test for connector 8/32, con-8.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
  Proximity test for connector 9/32, con-9.
    Connector dimension changed from 4 to 15, avg. spacing changed from 1.26705 to 0.271511
  Proximity test for connector 10/32, con-10.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
  Proximity test for connector 11/32, con-12.
  Proximity test for connector 12/32, con-13.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
  Proximity test for connector 13/32, con-16.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
  Proximity test for connector 14/32, con-17.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
  Proximity test for connector 15/32, con-20.
  Proximity test for connector 16/32, con-21.
    Connector dimension changed from 4 to 15, avg. spacing changed from 0.535476 to 0.114745
  Proximity test for connector 17/32, con-22.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
  Proximity test for connector 18/32, con-23.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
  Proximity test for connector 19/32, con-24.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
  Proximity test for connector 20/32, con-25.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
  Proximity test for connector 21/32, con-26.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
  Proximity test for connector 22/32, con-27.
  Proximity test for connector 23/32, con-28.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
  Proximity test for connector 24/32, con-29.
    Connector dimension changed from 4 to 15, avg. spacing changed from 0.506821 to 0.108604
  Proximity test for connector 25/32, con-30.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
  Proximity test for connector 26/32, con-32.
  Proximity test for connector 27/32, con-33.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
  Proximity test for connector 28/32, con-36.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
  Proximity test for connector 29/32, con-37.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
  Proximity test for connector 30/32, con-40.
  Proximity test for connector 31/32, con-41.
    Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952
  Proximity test for connector 32/32, con-42.
    Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 15
Connector con-2 current dim = 15
Connector con-3 current dim = 15
Connector con-4 current dim = 15
Connector con-5 current dim = 15
Connector con-6 current dim = 15
Connector con-7 current dim = 3
Connector con-8 current dim = 15
Connector con-9 current dim = 15
Connector con-10 current dim = 15
Connector con-12 current dim = 3
Connector con-13 current dim = 15
Connector con-16 current dim = 15
Connector con-17 current dim = 15
Connector con-20 current dim = 3
Connector con-21 current dim = 15
Connector con-22 current dim = 15
Connector con-23 current dim = 15
Connector con-24 current dim = 15
Connector con-25 current dim = 15
Connector con-26 current dim = 15
Connector con-27 current dim = 3
Connector con-28 current dim = 15
Connector con-29 current dim = 15
Connector con-30 current dim = 15
Connector con-32 current dim = 3
Connector con-33 current dim = 15
Connector con-36 current dim = 15
Connector con-37 current dim = 15
Connector con-40 current dim = 3
Connector con-41 current dim = 15
Connector con-42 current dim = 15
Domain list has 18 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 8.32902e-05
Number of periodic target domains = 0
Unstructured domain 1 of 18:
  boundary name = Wing1.
    Creating boundary name Wing1
Unstructured domain 2 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 3 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 4 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 5 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 6 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 7 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 8 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 9 of 18:
  boundary name = Wing2.
    Creating boundary name Wing2
Unstructured domain 10 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 11 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 12 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 13 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 14 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 15 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 16 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 17 of 18:
  boundary name = Farfield.
    Creating boundary name Farfield
Unstructured domain 18 of 18:
  boundary name = Farfield.
    Farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 18 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 18 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Sat Jul 02 2022  6:58:45AM EDT
Run Time: 00 Hours 00 Minutes 07 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Sat Jul 02 2022  6:58:45AM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 96 / 96 curves to EGADS originals
GMA contains 32 edge groups
GMA contains 18 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Sat Jul 02 2022  6:58:51AM EDT
Export Time: 00 Hours 00 Minutes 06 Seconds
Volume mesh:
	Number of nodes          = 16356
	Number of elements       = 95585
	Number of triangles      = 2982
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 95585
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 547
	Number of elements = 1090
	Number of tris = 1090
	Number of quad = 0
Body = 2
	Number of nodes    = 555
	Number of elements = 1106
	Number of tris = 1106
	Number of quad = 0
Body = 3
	Number of nodes    = 395
	Number of elements = 786
	Number of tris = 786
	Number of quad = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.1) "


Running SU2......
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='pyCAPS_SU2_Pointwise.cfg' mode='r' encoding='UTF-8'>
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==3792212== Warning: invalid file descriptor 1048564 in syscall close()
==3792212== Warning: invalid file descriptor 1048565 in syscall close()
==3792212== Warning: invalid file descriptor 1048566 in syscall close()
==3792212== Warning: invalid file descriptor 1048567 in syscall close()
==3792212==    Use --log-fd=<number> to select an alternative log fd.
==3792212== Warning: invalid file descriptor 1048568 in syscall close()
==3792212== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_2 (0, 0, 0).
   - BC_3 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_2, BC_3.
Input mesh file name: ../pointwise/caps.GeomToMesh.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_Pointwise.dat.
Surface file name: surface_flow_pyCAPS_SU2_Pointwise.
Volume file name: flow_pyCAPS_SU2_Pointwise.
Restart file name: restart_flow_pyCAPS_SU2_Pointwise.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_2|
|                                   |                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
16356 grid points.
95585 volume elements.
3 surface markers.
786 boundary elements in index 0 (Marker = BC_1).
1090 boundary elements in index 1 (Marker = BC_2).
1106 boundary elements in index 2 (Marker = BC_3).
95585 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.11289e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 6570.86. Mean K: 103.587. Standard deviation K: 505.135.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        47.0293|        82.9833|
|     CV Face Area Aspect Ratio|        1.06486|        89.2124|
|           CV Sub-Volume Ratio|        1.10228|        2729.83|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     16356|    1/1.00|        10|
|         1|      2589|    1/6.32|   8.11415|
|         2|       366|    1/7.07|   6.34041|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 89.961 m^2.
Area projection in the x-plane = 8.28857 m^2, y-plane = 3.66354 m^2, z-plane = 42.3644 m^2.
Max. coordinate in the x-direction = 12.3619 m, y-direction = 7.07107 m, z-direction = 0.510646 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.368435 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_2 is NOT a single plane.
Boundary marker BC_3 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.1170e+00|    0.442811|    2.860057|    2.406125|    5.933707|    2.248402|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.0598e+00|    0.176999|    2.668496|    2.387415|    5.662704|    2.704922|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.0410e+00|    0.135584|    2.666990|    2.525093|    5.611667|    3.652092|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.0336e+00|    0.077267|    2.655221|    2.592937|    5.549155|    4.812433|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0393e+00|    0.001555|    2.649759|    2.604525|    5.479770|    5.688183|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|    0.00155504|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Pointwise.dat|
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_Pointwise.csv|

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).
|Tecplot binary                     |flow_pyCAPS_SU2_Pointwise.szplt    |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_SU2_Pointwise.szplt|

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).

------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  0.627084 Cd =  0.110243
Cmx =  0.000149 Cmy =  -0.184427 Cmz =  0.000345
Cx =  0.099282 Cy =  9e-05 Cz =  0.628913
==3789150== 
==3789150== HEAP SUMMARY:
==3789150==     in use at exit: 4,308,616 bytes in 24,764 blocks
==3789150==   total heap usage: 727,189 allocs, 702,425 frees, 494,576,284 bytes allocated
==3789150== 
==3789150== LEAK SUMMARY:
==3789150==    definitely lost: 0 bytes in 0 blocks
==3789150==    indirectly lost: 0 bytes in 0 blocks
==3789150==      possibly lost: 0 bytes in 0 blocks
==3789150==    still reachable: 0 bytes in 0 blocks
==3789150==         suppressed: 4,308,616 bytes in 24,764 blocks
==3789150== 
==3789150== For lists of detected and suppressed errors, rerun with: -s
==3789150== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1842 from 1842)
97.95user 3.78system 1:41.55elapsed 100%CPU (0avgtext+0avgdata 323680maxresident)k
15168inputs+40432outputs (106major+635494minor)pagefaults 0swaps

real	1m41.563s
user	1m37.962s
sys	0m3.803s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_pointwise_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_and_Tetgen_PyTest.py test;'
su2_and_Tetgen_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_Tetgen_PyTest.py -outLevel=0
==3806700== Memcheck, a memory error detector
==3806700== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==3806700== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==3806700== Command: python -u su2_and_Tetgen_PyTest.py -outLevel=0
==3806700== 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 267
Number of elements = 530
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3139
Total number of elements = 6266

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface nodes - 3139
Number of surface elements - 6266
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds:  1.07045
Creating surface mesh ...
Surface mesh seconds:  0.227342
Recovering boundaries...
Boundary recovery seconds:  3.07841
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.115651
Suppressing Steiner points ...
Steiner suppression seconds:  0.00037
Recovering Delaunayness...
Delaunay recovery seconds:  0.419902
Refining mesh...
  4188 insertions, added 2100 points, 134662 tetrahedra in queue.
  1394 insertions, added 425 points, 138812 tetrahedra in queue.
  1858 insertions, added 471 points, 136161 tetrahedra in queue.
  2477 insertions, added 507 points, 118959 tetrahedra in queue.
  3302 insertions, added 481 points, 64039 tetrahedra in queue.
  4401 insertions, added 394 points, 1342 tetrahedra in queue.
Refinement seconds:  25.4463
Smoothing vertices...
Mesh smoothing seconds:  17.4245
Improving mesh...
Mesh improvement seconds:  0.549696
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.05973
Total running seconds:  48.4275

Statistics:

  Input points: 3139
  Input facets: 6266
  Input segments: 9399
  Input holes: 2
  Input regions: 0

  Mesh points: 8009
  Mesh tetrahedra: 39254
  Mesh faces: 81642
  Mesh faces on exterior boundary: 6268
  Mesh faces on input facets: 6268
  Mesh edges on input segments: 9400
  Steiner points on input segments:  1
  Steiner points inside domain: 4869

Done meshing using TetGen!
Volume mesher added surface elements - data transfer will NOT be possible.
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.1) "


Running SU2......
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='pyCAPS_SU2_Tetgen.cfg' mode='r' encoding='UTF-8'>
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==3832204== Warning: invalid file descriptor 1048564 in syscall close()
==3832204== Warning: invalid file descriptor 1048565 in syscall close()
==3832204== Warning: invalid file descriptor 1048566 in syscall close()
==3832204== Warning: invalid file descriptor 1048567 in syscall close()
==3832204==    Use --log-fd=<number> to select an alternative log fd.
==3832204== Warning: invalid file descriptor 1048568 in syscall close()
==3832204== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_0.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_Tetgen.dat.
Surface file name: surface_flow_pyCAPS_SU2_Tetgen.
Volume file name: flow_pyCAPS_SU2_Tetgen.
Restart file name: restart_flow_pyCAPS_SU2_Tetgen.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
8009 grid points.
39254 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
530 boundary elements in index 2 (Marker = BC_3).
39254 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.09074e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.561. Standard deviation K: 37.5336.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.05157|        83.9276|
|     CV Face Area Aspect Ratio|        1.31853|        36832.6|
|           CV Sub-Volume Ratio|         1.0328|    1.76867e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8009|    1/1.00|        10|
|         1|      1339|    1/5.98|    8.2634|
|         2|       221|    1/6.06|   6.79914|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  5.8933e-01|    0.620196|    3.052156|    2.095402|    6.111091|    1.821394|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  5.9083e-01|    0.861155|    3.388133|    3.046216|    6.371496|    2.187054|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  5.5059e-01|    0.750173|    3.392367|    3.289072|    6.260635|    3.214764|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  5.2671e-01|    0.570309|    3.263082|    3.330629|    6.049566|    4.586176|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  5.1429e-01|    0.568946|    3.182696|    3.257588|    6.036569|    5.762812|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.568946|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Tetgen.dat |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_Tetgen.csv |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview                           |flow_pyCAPS_SU2_Tetgen.vtu         |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface                   |surface_flow_pyCAPS_SU2_Tetgen.vtu |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).

------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  0.75489 Cd =  0.130993
Cmx =  -0.007921 Cmy =  -0.211909 Cmz =  0.002289
Cx =  0.117799 Cy =  0.001444 Cz =  0.757061
==3806700== 
==3806700== HEAP SUMMARY:
==3806700==     in use at exit: 4,287,941 bytes in 24,709 blocks
==3806700==   total heap usage: 942,664 allocs, 917,955 frees, 629,029,554 bytes allocated
==3806700== 
==3806700== LEAK SUMMARY:
==3806700==    definitely lost: 0 bytes in 0 blocks
==3806700==    indirectly lost: 0 bytes in 0 blocks
==3806700==      possibly lost: 0 bytes in 0 blocks
==3806700==    still reachable: 0 bytes in 0 blocks
==3806700==         suppressed: 4,287,941 bytes in 24,709 blocks
==3806700== 
==3806700== For lists of detected and suppressed errors, rerun with: -s
==3806700== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1865 from 1865)
165.64user 2.08system 2:49.68elapsed 98%CPU (0avgtext+0avgdata 365916maxresident)k
0inputs+23608outputs (0major+599121minor)pagefaults 0swaps

real	2m49.692s
user	2m45.644s
sys	0m2.095s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_X43a_PyTest.py test;'
su2_X43a_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_X43a_PyTest.py -outLevel=0
==3832568== Memcheck, a memory error detector
==3832568== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==3832568== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==3832568== Command: python -u su2_X43a_PyTest.py -outLevel=0
==3832568== 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 3808
Number of elements = 7616
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 5653
Number of elements = 11302
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11302
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9461
Total number of elements = 18918

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Number of surface nodes - 9461
Number of surface elements - 18918
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds:  2.72131
Creating surface mesh ...
Surface mesh seconds:  0.692996
Recovering boundaries...
Warning:  6 segments are not recovered.
Boundary recovery seconds:  8.04928
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.209533
Suppressing Steiner points ...
Steiner suppression seconds:  0.000419
Recovering Delaunayness...
Delaunay recovery seconds:  1.13532
Refining mesh...
  12616 insertions, added 5170 points, 18149 tetrahedra in queue.
Refinement seconds:  23.1553
Smoothing vertices...
Mesh smoothing seconds:  18.7269
Improving mesh...
Mesh improvement seconds:  0.850108
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.113516
Total running seconds:  55.8959

Statistics:

  Input points: 9461
  Input facets: 18918
  Input segments: 28377
  Input holes: 1
  Input regions: 0

  Mesh points: 14832
  Mesh tetrahedra: 61120
  Mesh faces: 131702
  Mesh faces on exterior boundary: 18924
  Mesh faces on input facets: 18924
  Mesh edges on input segments: 28380
  Steiner points on input segments:  3
  Steiner points inside domain: 5368

Done meshing using TetGen!
Volume mesher added surface elements - data transfer will NOT be possible.
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - x43A
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.1) "


Running SU2......
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='x43a_Test.cfg' mode='r' encoding='UTF-8'>
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==3867126== Warning: invalid file descriptor 1048564 in syscall close()
==3867126== Warning: invalid file descriptor 1048565 in syscall close()
==3867126== Warning: invalid file descriptor 1048566 in syscall close()
==3867126== Warning: invalid file descriptor 1048567 in syscall close()
==3867126==    Use --log-fd=<number> to select an alternative log fd.
==3867126== Warning: invalid file descriptor 1048568 in syscall close()
==3867126== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../myMesh/tetgen_0.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_x43a_Test.dat.
Surface file name: surface_flow_x43a_Test.
Volume file name: flow_x43a_Test.
Restart file name: restart_flow_x43a_Test.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
14832 grid points.
61120 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11302 boundary elements in index 1 (Marker = BC_2).
61120 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.525189. Standard deviation K: 2.58.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.85426|        83.9017|
|     CV Face Area Aspect Ratio|        1.82697|        18175.5|
|           CV Sub-Volume Ratio|              1|    2.40648e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14832|    1/1.00|        10|
|         1|      2681|    1/5.53|   8.48119|
|         2|       491|    1/5.46|   7.22453|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13596.7 m^2.
Area projection in the x-plane = 761.677 m^2, y-plane = 2062.48 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        916077|             1|   m^2/s^2|        916077|
|            Velocity-X|       1189.41|             1|       m/s|       1189.41|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       62.3342|             1|       m/s|       62.3342|
|    Velocity Magnitude|       1191.04|             1|       m/s|       1191.04|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.0340e+00|    2.731643|    5.665683|    4.729371|    8.731119|   -0.364357|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.4653e-01|    3.080507|    6.130761|    5.704829|    9.099189|   -0.114402|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.4631e-01|    3.238998|    6.327615|    5.859548|    9.209446|   -0.043482|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  9.2101e-01|    3.256395|    6.327390|    5.786152|    9.234758|   -0.032063|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  9.0419e-01|    3.162813|    6.212532|    5.616824|    9.137964|   -0.051711|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.16281|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_x43a_Test.dat         |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|CSV file                           |surface_flow_x43a_Test.csv         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview                           |flow_x43a_Test.vtu                 |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview surface                   |surface_flow_x43a_Test.vtu         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
Warning: there are 124 non-physical points in the solution.
Warning: 597 reconstructed states for upwinding are non-physical.

------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  -5.932185 Cd =  114.717353
Cmx =  38.748728 Cmy =  9154.23677 Cmz =  207.157404
Cx =  114.870603 Cy =  0.839477 Cz =  0.079788
==3832568== 
==3832568== HEAP SUMMARY:
==3832568==     in use at exit: 4,286,395 bytes in 24,705 blocks
==3832568==   total heap usage: 5,851,391 allocs, 5,826,686 frees, 4,882,260,964 bytes allocated
==3832568== 
==3832568== LEAK SUMMARY:
==3832568==    definitely lost: 0 bytes in 0 blocks
==3832568==    indirectly lost: 0 bytes in 0 blocks
==3832568==      possibly lost: 0 bytes in 0 blocks
==3832568==    still reachable: 0 bytes in 0 blocks
==3832568==         suppressed: 4,286,395 bytes in 24,705 blocks
==3832568== 
==3832568== For lists of detected and suppressed errors, rerun with: -s
==3832568== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1865 from 1865)
533.86user 6.76system 9:06.68elapsed 98%CPU (0avgtext+0avgdata 576128maxresident)k
0inputs+35896outputs (0major+1930369minor)pagefaults 0swaps

real	9m6.688s
user	8m53.864s
sys	0m6.781s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==3867318== Memcheck, a memory error detector
==3867318== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==3867318== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==3867318== Command: python -u cart3d_PyTest.py -outLevel=0
==3867318== 
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 7.674092
 Tessellating body 1 with  MaxEdge = 0.191852  Sag = 0.007674  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9  > autoInputs.out
 Executing: ./aero.csh > aero.out
C_A  0.13545895
C_Y  -0.0023190349
C_N  0.0017662912
C_D  0.13543807
C_S  -0.0023190349
C_L  -0.002962234
C_l  -0.00170699
C_m  -0.00604561
C_n  0.0354751
C_M_x  -0.00046789
C_M_y  -0.00604561
C_M_z  0.0355131
==3867318== 
==3867318== HEAP SUMMARY:
==3867318==     in use at exit: 4,058,949 bytes in 24,316 blocks
==3867318==   total heap usage: 532,049 allocs, 507,733 frees, 466,622,828 bytes allocated
==3867318== 
==3867318== LEAK SUMMARY:
==3867318==    definitely lost: 0 bytes in 0 blocks
==3867318==    indirectly lost: 0 bytes in 0 blocks
==3867318==      possibly lost: 0 bytes in 0 blocks
==3867318==    still reachable: 0 bytes in 0 blocks
==3867318==         suppressed: 4,058,949 bytes in 24,316 blocks
==3867318== 
==3867318== For lists of detected and suppressed errors, rerun with: -s
==3867318== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1837 from 1837)
88.09user 2.13system 1:02.57elapsed 144%CPU (0avgtext+0avgdata 296808maxresident)k
0inputs+17600outputs (0major+350277minor)pagefaults 0swaps

real	1m2.576s
user	1m28.098s
sys	0m2.138s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
==3868349== Memcheck, a memory error detector
==3868349== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==3868349== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==3868349== Command: python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
==3868349== 
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/exec_comp.py:7: DeprecationWarning: `np.complex` is a deprecated alias for the builtin `complex`. To silence this warning, use `complex` by itself. Doing this will not modify any behavior and is safe. If you specifically wanted the numpy scalar type, use `np.complex128` here.
Deprecated in NumPy 1.20; for more details and guidance: https://numpy.org/devdocs/release/1.20.0-notes.html#deprecations
  from numpy import ndarray, imag, complex as npcomplex
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/external_code_comp.py:6: DeprecationWarning: 

  `numpy.distutils` is deprecated since NumPy 1.23.0, as a result
  of the deprecation of `distutils` itself. It will be removed for
  Python >= 3.12. For older Python versions it will remain present.
  It is recommended to use `setuptools < 60.0` for those Python versions.
  For more details, see:
    https://numpy.org/devdocs/reference/distutils_status_migration.html 


  import numpy.distutils
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/surrogate_models/response_surface.py:7: DeprecationWarning: The module numpy.dual is deprecated.  Instead of using dual, use the functions directly from numpy or scipy.
  from numpy.dual import lstsq
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/pyDOE2/doe_factorial.py:16: DeprecationWarning: the imp module is deprecated in favour of importlib; see the module's documentation for alternative uses
  import imp
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 10.084180
 Tessellating body 1 with  MaxEdge = 0.252104  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7  -mesh2d > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:17:16) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
   (07:17:18) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
alpha [2.]  CL2 [0.1057817]  CL 0.3252412
alpha [2.]  CL2 [0.1057817]  CL 0.3252412
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:17:24) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
   (07:17:28) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:17:28) Linearizing cut-cells
   (07:17:28) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:17:28) Computing gradients
   (07:17:32) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10602001]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  1.05782D-01    |proj g|=  1.06020D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:17:38) Running aero.csh on 4 core(s) in M0.5901A1.89398B0_DP1
   (07:17:40) aero.csh done
 o case M0.5901A1.89398B0_DP1, averaging data over 1 cycle(s)
alpha [1.89397999]  CL2 [0.09478706]  CL 0.30787504
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:17:43) Running aero.csh on 4 core(s) in M0.5901A1.89398B0_DP1
   (07:17:47) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:17:47) Linearizing cut-cells
   (07:17:47) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:17:47) Computing gradients
   (07:17:51) ... done
 o case M0.5901A1.89398B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10074813]]

At iterate    1    f=  9.47871D-02    |proj g|=  1.00748D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:17:55) Running aero.csh on 4 core(s) in M0.5901A-0.132111B0_DP1
   (07:17:58) aero.csh done
 o case M0.5901A-0.132111B0_DP1, averaging data over 1 cycle(s)
alpha [-0.13211104]  CL2 [0.00047434]  CL -0.02139385
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:18:01) Running aero.csh on 4 core(s) in M0.5901A-0.132111B0_DP1
   (07:18:05) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:18:05) Linearizing cut-cells
   (07:18:05) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:18:06) Computing gradients
   (07:18:10) ... done
 o case M0.5901A-0.132111B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00732582]]

At iterate    2    f=  4.74339D-04    |proj g|=  7.32582D-03
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:18:13) Running aero.csh on 4 core(s) in M0.5901A0.00522812B0_DP1
   (07:18:15) aero.csh done
 o case M0.5901A0.00522812B0_DP1, averaging data over 1 cycle(s)
alpha [0.00522812]  CL2 [1.32465164e-05]  CL 0.00361761
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:18:18) Running aero.csh on 4 core(s) in M0.5901A0.00522812B0_DP1
   (07:18:23) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:18:23) Linearizing cut-cells
   (07:18:23) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:18:23) Computing gradients
   (07:18:27) ... done
 o case M0.5901A0.00522812B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.001238]]

At iterate    3    f=  1.32465D-05    |proj g|=  1.23800D-03
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:18:33) Running aero.csh on 4 core(s) in M0.5901A-0.0146258B0_DP1
   (07:18:36) aero.csh done
 o case M0.5901A-0.0146258B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01462583]  CL2 [2.89471283e-05]  CL -0.00546528
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:18:39) Running aero.csh on 4 core(s) in M0.5901A-0.0146258B0_DP1
   (07:18:43) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:18:43) Linearizing cut-cells
   (07:18:43) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:18:43) Computing gradients
   (07:18:47) ... done
 o case M0.5901A-0.0146258B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00180066]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:18:50) Running aero.csh on 4 core(s) in M0.5901A0.000671285B0_DP1
   (07:18:53) aero.csh done
 o case M0.5901A0.000671285B0_DP1, averaging data over 1 cycle(s)
alpha [0.00067128]  CL2 [8.15511616e-06]  CL 0.00278569
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:18:57) Running aero.csh on 4 core(s) in M0.5901A0.000671285B0_DP1
   (07:19:01) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:19:01) Linearizing cut-cells
   (07:19:01) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:19:01) Computing gradients
   (07:19:05) ... done
 o case M0.5901A0.000671285B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00097886]]

At iterate    4    f=  8.15512D-06    |proj g|=  9.78864D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:19:09) Running aero.csh on 4 core(s) in M0.5901A-0.0165419B0_DP1
   (07:19:11) aero.csh done
 o case M0.5901A-0.0165419B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01654192]  CL2 [3.33627463e-05]  CL -0.00584049
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:19:15) Running aero.csh on 4 core(s) in M0.5901A-0.0165419B0_DP1
   (07:19:19) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:19:19) Linearizing cut-cells
   (07:19:19) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:19:19) Computing gradients
   (07:19:23) ... done
 o case M0.5901A-0.0165419B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00193604]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:19:26) Running aero.csh on 4 core(s) in M0.5901A-0.00140463B0_DP1
   (07:19:29) aero.csh done
 o case M0.5901A-0.00140463B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00140463]  CL2 [6.12816493e-06]  CL 0.00237962
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:19:33) Running aero.csh on 4 core(s) in M0.5901A-0.00140463B0_DP1
   (07:19:38) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:19:38) Linearizing cut-cells
   (07:19:38) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:19:39) Computing gradients
   (07:19:43) ... done
 o case M0.5901A-0.00140463B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00084715]]

At iterate    5    f=  6.12816D-06    |proj g|=  8.47152D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:19:48) Running aero.csh on 4 core(s) in M0.5901A-0.0147565B0_DP1
   (07:19:51) aero.csh done
 o case M0.5901A-0.0147565B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01475651]  CL2 [2.9240213e-05]  CL -0.00549114
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:19:56) Running aero.csh on 4 core(s) in M0.5901A-0.0147565B0_DP1
   (07:19:59) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:20:00) Linearizing cut-cells
   (07:20:00) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:20:00) Computing gradients
   (07:20:04) ... done
 o case M0.5901A-0.0147565B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00181002]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:20:07) Running aero.csh on 4 core(s) in M0.5901A-0.00259716B0_DP1
   (07:20:10) aero.csh done
 o case M0.5901A-0.00259716B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00259716]  CL2 [5.08191983e-06]  CL 0.002137
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:20:13) Running aero.csh on 4 core(s) in M0.5901A-0.00259716B0_DP1
   (07:20:17) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:20:17) Linearizing cut-cells
   (07:20:17) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:20:17) Computing gradients
   (07:20:21) ... done
 o case M0.5901A-0.00259716B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00077084]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:20:25) Running aero.csh on 4 core(s) in M0.5901A-0.00367151B0_DP1
   (07:20:28) aero.csh done
 o case M0.5901A-0.00367151B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00367151]  CL2 [4.27119297e-06]  CL 0.00192854
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:20:32) Running aero.csh on 4 core(s) in M0.5901A-0.00367151B0_DP1
   (07:20:36) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:20:36) Linearizing cut-cells
   (07:20:36) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:20:36) Computing gradients
   (07:20:40) ... done
 o case M0.5901A-0.00367151B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00070603]]

At iterate    6    f=  4.27119D-06    |proj g|=  7.06030D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:20:43) Running aero.csh on 4 core(s) in M0.5901A-0.0150127B0_DP1
   (07:20:46) aero.csh done
 o case M0.5901A-0.0150127B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01501269]  CL2 [2.98325477e-05]  CL -0.00554238
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:20:50) Running aero.csh on 4 core(s) in M0.5901A-0.0150127B0_DP1
   (07:20:53) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:20:54) Linearizing cut-cells
   (07:20:54) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:20:54) Computing gradients
   (07:20:58) ... done
 o case M0.5901A-0.0150127B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00182884]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:21:01) Running aero.csh on 4 core(s) in M0.5901A-0.00433344B0_DP1
   (07:21:04) aero.csh done
 o case M0.5901A-0.00433344B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00433344]  CL2 [3.77191769e-06]  CL 0.00179209
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:21:08) Running aero.csh on 4 core(s) in M0.5901A-0.00433344B0_DP1
   (07:21:12) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:21:12) Linearizing cut-cells
   (07:21:12) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:21:12) Computing gradients
   (07:21:16) ... done
 o case M0.5901A-0.00433344B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00066572]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:21:19) Running aero.csh on 4 core(s) in M0.5901A-0.004888B0_DP1
   (07:21:22) aero.csh done
 o case M0.5901A-0.004888B0_DP1, averaging data over 1 cycle(s)
alpha [-0.004888]  CL2 [3.36327638e-06]  CL 0.00167372
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:21:25) Running aero.csh on 4 core(s) in M0.5901A-0.004888B0_DP1
   (07:21:28) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (07:21:29) Linearizing cut-cells
   (07:21:29) ... done
   o Number of simultaneous xsensit jobs:  1
   (07:21:29) Computing gradients
   (07:21:33) ... done
 o case M0.5901A-0.004888B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00062781]]

At iterate    7    f=  3.36328D-06    |proj g|=  6.27809D-04

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      7     14      7     0     0   6.278D-04   3.363D-06
  F =   3.3632763807999997E-006

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized value: [-0.004888]
==3868349== 
==3868349== HEAP SUMMARY:
==3868349==     in use at exit: 6,418,417 bytes in 39,022 blocks
==3868349==   total heap usage: 7,282,456 allocs, 7,243,434 frees, 7,363,188,553 bytes allocated
==3868349== 
==3868349== LEAK SUMMARY:
==3868349==    definitely lost: 0 bytes in 0 blocks
==3868349==    indirectly lost: 0 bytes in 0 blocks
==3868349==      possibly lost: 0 bytes in 0 blocks
==3868349==    still reachable: 0 bytes in 0 blocks
==3868349==                       of which reachable via heuristic:
==3868349==                         stdstring          : 38 bytes in 1 blocks
==3868349==         suppressed: 6,418,417 bytes in 39,022 blocks
==3868349== 
==3868349== For lists of detected and suppressed errors, rerun with: -s
==3868349== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 4478 from 4478)
588.70user 30.91system 9:22.43elapsed 110%CPU (0avgtext+0avgdata 568872maxresident)k
18232inputs+171296outputs (77major+3939314minor)pagefaults 0swaps

real	9m22.442s
user	9m48.716s
sys	0m30.937s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;'
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==3894044== Memcheck, a memory error detector
==3894044== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==3894044== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==3894044== Command: python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
==3894044== 
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/exec_comp.py:7: DeprecationWarning: `np.complex` is a deprecated alias for the builtin `complex`. To silence this warning, use `complex` by itself. Doing this will not modify any behavior and is safe. If you specifically wanted the numpy scalar type, use `np.complex128` here.
Deprecated in NumPy 1.20; for more details and guidance: https://numpy.org/devdocs/release/1.20.0-notes.html#deprecations
  from numpy import ndarray, imag, complex as npcomplex
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/external_code_comp.py:6: DeprecationWarning: 

  `numpy.distutils` is deprecated since NumPy 1.23.0, as a result
  of the deprecation of `distutils` itself. It will be removed for
  Python >= 3.12. For older Python versions it will remain present.
  It is recommended to use `setuptools < 60.0` for those Python versions.
  For more details, see:
    https://numpy.org/devdocs/reference/distutils_status_migration.html 


  import numpy.distutils
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/surrogate_models/response_surface.py:7: DeprecationWarning: The module numpy.dual is deprecated.  Instead of using dual, use the functions directly from numpy or scipy.
  from numpy.dual import lstsq
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/pyDOE2/doe_factorial.py:16: DeprecationWarning: the imp module is deprecated in favour of importlib; see the module's documentation for alternative uses
  import imp
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 10.084443
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:26:04) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:26:14) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [1. 2.]  CL2 [0.04745667]  CL -0.217845
twist [1. 2.]  CL2 [0.04745667]  CL -0.217845
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:26:27) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:26:44) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (07:26:44) Linearizing cut-cells
   (07:26:46) ... done
   o Number of simultaneous xsensit jobs:  2
   (07:26:46) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (07:26:50) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02768712 0.02710382]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            2     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.74567D-02    |proj g|=  2.76871D-02
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084443
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:27:01) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:27:13) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [0.97231288 1.97289618]  CL2 [0.04578804]  CL -0.213981
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:27:26) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:27:44) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (07:27:45) Linearizing cut-cells
   (07:27:47) ... done
   o Number of simultaneous xsensit jobs:  2
   (07:27:47) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (07:27:51) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02718156 0.02662519]]

At iterate    1    f=  4.57880D-02    |proj g|=  2.71816D-02
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084427
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:28:00) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:28:10) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.51633339  0.46520815]  CL2 [2.2250932e-05]  CL 0.00471709
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:28:24) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:28:41) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (07:28:41) Linearizing cut-cells
   (07:28:43) ... done
   o Number of simultaneous xsensit jobs:  2
   (07:28:43) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (07:28:47) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[-0.00061004 -0.0005932 ]]

At iterate    2    f=  2.22509D-05    |proj g|=  6.10038D-04
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084427
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:28:56) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:29:08) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.48365701  0.49806686]  CL2 [5.12277885e-08]  CL -0.00022634
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:29:21) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:29:36) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (07:29:37) Linearizing cut-cells
   (07:29:39) ... done
   o Number of simultaneous xsensit jobs:  2
   (07:29:39) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (07:29:43) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[2.92772918e-05 2.84940456e-05]]

At iterate    3    f=  5.12278D-08    |proj g|=  2.92773D-05
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084427
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:29:53) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:30:03) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.48515341  0.49656084]  CL2 [1.3226687e-09]  CL -3.637e-05
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (07:30:15) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (07:30:31) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (07:30:32) Linearizing cut-cells
   (07:30:34) ... done
   o Number of simultaneous xsensit jobs:  2
   (07:30:34) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (07:30:38) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[4.70490486e-06 4.57899611e-06]]

At iterate    4    f=  1.32267D-09    |proj g|=  4.70490D-06

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    2      4      5      4     0     0   4.705D-06   1.323D-09
  F =   1.3226687019000001E-009

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.48515341  0.49656084]
==3894044== 
==3894044== HEAP SUMMARY:
==3894044==     in use at exit: 6,417,676 bytes in 39,022 blocks
==3894044==   total heap usage: 6,018,510 allocs, 5,979,488 frees, 6,652,321,471 bytes allocated
==3894044== 
==3894044== LEAK SUMMARY:
==3894044==    definitely lost: 0 bytes in 0 blocks
==3894044==    indirectly lost: 0 bytes in 0 blocks
==3894044==      possibly lost: 0 bytes in 0 blocks
==3894044==    still reachable: 0 bytes in 0 blocks
==3894044==                       of which reachable via heuristic:
==3894044==                         stdstring          : 38 bytes in 1 blocks
==3894044==         suppressed: 6,417,676 bytes in 39,022 blocks
==3894044== 
==3894044== For lists of detected and suppressed errors, rerun with: -s
==3894044== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 4494 from 4494)
805.60user 21.26system 9:04.70elapsed 151%CPU (0avgtext+0avgdata 567204maxresident)k
103200inputs+144328outputs (60major+3103337minor)pagefaults 0swaps

real	9m4.708s
user	13m25.606s
sys	0m21.280s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected)
=================================================


*************************************************
*************************************************

=================================================
Did not run examples for:

Fun3D
=================================================

All tests pass!

+ exit 0
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Sleeping for 5 seconds due to JENKINS-32191...
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/CFD,LINUX64,reynolds)
[Static Analysis] Using reference build 'ESP_ValgrindCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #178' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_ValgrindCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #181'.
[Checks API] No suitable checks publisher found.
[Valgrind] Files to copy:
[Valgrind] Analysing valgrind results
[Valgrind] Ending the valgrind analysis.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS